Patents by Inventor Marco Pieri
Marco Pieri has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Publication number: 20230093896Abstract: A rotary machine assembly for a turbomachine, such as a rotor, having a rotor wheel where a plurality of circumferentially spaced female dovetail slots are obtained. The rotary machine assembly also comprises a plurality of blades. Between each blade and the adjacent one there is an interface angle. Each blade comprises a male dovetail, configured to fit with a corresponding female dovetail slot of the rotor wheel along an insertion direction. The female dovetail slots are shaped so that the insertion direction of each male dovetail is convergent with the rotation axis of the rotor wheel, so as to form with it an insertion angle, so as to insert gradually all the male dovetails into the female dovetail slots and packing them also gradually. A method for assembling a rotary machine assembly, which does not require any specific tool, is also disclosed.Type: ApplicationFiled: February 18, 2021Publication date: March 30, 2023Inventor: Marco PIERI
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Patent number: 10669868Abstract: Fixing set for securely assembling and locking a blade shaped element, for instance a turbine blade, on a support, for instance a turbine rotor. The blade shaped element is adapted to be inserted into a groove of the external surface of the support and the fixing set includes first, second and third locking elements adapted to be inserted into the groove, between the lower end surface of the root portion of the blade shaped element and the groove base surface. The first, second and third locking elements are adapted to securely lock the blade shaped element on the support and are further adapted to allow easy and simple installation by an operator with no need of additional working and extra machining.Type: GrantFiled: December 21, 2017Date of Patent: June 2, 2020Assignee: NUOVO PIGNONE TECNOLOGIE SRLInventor: Marco Pieri
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Publication number: 20200141261Abstract: The sealing system (1) for a machine comprises: a sealing element (4) that is movable back and forth along a direction (D) and that comprises a first recess (41) with first and second surfaces (42, 43), a component (2) of an assembly of the machine that comprises a second recess (21) with first and second surfaces (22, 23), and an elastic element (5). The first and second recesses (41, 21) face each other. The elastic element (5) is partially housed inside the first recess (41) and partially housed inside the second recess (21) so to apply forces on the first and second surfaces (42, 22, 43, 23) depending on where the sealing element (4) is positioned with respect to the component (2).Type: ApplicationFiled: July 2, 2018Publication date: May 7, 2020Inventor: Marco PIERI
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Patent number: 10641131Abstract: A valve assembly for use to regulate a flow of steam in a flowpath of a turbine. The valve assembly can be configured with a body that circumscribes a rotor. The body is disposed upstream of the rotor blades. In one implementation, the body forms an annular ring with a plurality of arcuate segments, each being configured to move independently of the other segments in the ring to change the size of an annular gap between the arcuate segments and the rotor. The size of the annular gap corresponds with flow parameters for working fluid that flows across the rotor and that exits the turbine for use in pre-heaters and like collateral equipment.Type: GrantFiled: June 25, 2018Date of Patent: May 5, 2020Assignee: Nuovo Pignone S.R.L.Inventor: Marco Pieri
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Patent number: 10619502Abstract: An expansion joint for sealingly connecting a first and a second turbine component having wall openings coaxial with fluid passages in relative displacement, the openings defining a recess with opposing axial surfaces acting as seat for the joint in the first and the second turbine component, the joint comprising a sealing ring adapted to be disposed in the recess such as to axially and radially engage with the recess surfaces around the fluid passages, an intermediate ring adapted for being interposed between the sealing ring and the radial surface of the first turbine component, wherein the intermediate ring has openings axially engaging with protuberances of the sealing ring to prevent relative rotation.Type: GrantFiled: December 15, 2017Date of Patent: April 14, 2020Assignee: NUOVO PIGNONE TECNOLOGIE SRLInventor: Marco Pieri
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Publication number: 20180298786Abstract: A valve assembly for use to regulate a flow of steam in a flowpath of a turbine. The valve assembly can be configured with a body that circumscribes a rotor. The body is disposed upstream of the rotor blades. In one implementation, the body forms an annular ring with a plurality of arcuate segments, each being configured to move independently of the other segments in the ring to change the size of an annular gap between the arcuate segments and the rotor. The size of the annular gap corresponds with flow parameters for working fluid that flows across the rotor and that exits the turbine for use in pre-heaters and like collateral equipment.Type: ApplicationFiled: June 25, 2018Publication date: October 18, 2018Inventor: Marco Pieri
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Patent number: 10082380Abstract: A tool to measure the radial stacking angle of a cylindrical blade comprises a base configured to indicate a radial direction of the hub, a component slidable over the blade and configured to indicate the stacking direction of the cylindrical blade, reference elements to provide a reference scale, a setting element configured to set the position of the component with respect to the base, a marker element configured to indicate the magnitude of the angle between the stacking direction and the radial direction using the reference elements; the angle corresponds to the radial stacking angle.Type: GrantFiled: November 28, 2014Date of Patent: September 25, 2018Assignee: Nuovo Pignone SRLInventor: Marco Pieri
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Patent number: 10030544Abstract: A valve assembly for use to regulate a flow of steam in a flowpath of a turbine. The valve assembly can be configured with a body that circumscribes a rotor. The body is disposed upstream of the rotor blades. In one implementation, the body forms an annular ring with a plurality of arcuate segments, each being configured to move independently of the other segments in the ring to change the size of an annular gap between the arcuate segments and the rotor. The size of the annular gap corresponds with flow parameters for working fluid that flows across the rotor and that exits the turbine for use in pre-heaters and like collateral equipment.Type: GrantFiled: December 22, 2015Date of Patent: July 24, 2018Assignee: Nuovo Pignone S.R.L.Inventor: Marco Pieri
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Publication number: 20180179903Abstract: Fixing set for securely assembling and locking a blade shaped element, for instance a turbine blade, on a support, for instance a turbine rotor. The blade shaped element is adapted to be inserted into a groove of the external surface of the support and the fixing set includes first, second and third locking elements adapted to be inserted into the groove, between the lower end surface of the root portion of the blade shaped element and the groove base surface. The first, second and third locking elements are adapted to securely lock the blade shaped element on the support and are further adapted to allow easy and simple installation by an operator with no need of additional working and extra machining.Type: ApplicationFiled: December 21, 2017Publication date: June 28, 2018Inventor: Marco PIERI
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Publication number: 20180171813Abstract: An expansion joint for sealingly connecting a first and a second turbine component having wall openings coaxial with fluid passages in relative displacement, the openings defining a recess with opposing axial surfaces acting as seat for the joint in the first and the second turbine component, the joint comprising a sealing ring adapted to be disposed in the recess such as to axially and radially engage with the recess surfaces around the fluid passages, an intermediate ring adapted for being interposed between the sealing ring and the radial surface of the first turbine component, wherein the intermediate ring has openings axially engaging with protuberances of the sealing ring to prevent relative rotation.Type: ApplicationFiled: December 15, 2017Publication date: June 21, 2018Inventor: Marco PIERI
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Publication number: 20170096913Abstract: A valve assembly for use to regulate a flow of steam in a flowpath of a turbine. The valve assembly can be configured with a body that circumscribes a rotor. The body is disposed upstream of the rotor blades. In one implementation, the body forms an annular ring with a plurality of arcuate segments, each being configured to move independently of the other segments in the ring to change the size of an annular gap between the arcuate segments and the rotor. The size of the annular gap corresponds with flow parameters for working fluid that flows across the rotor and that exits the turbine for use in pre-heaters and like collateral equipment.Type: ApplicationFiled: December 22, 2015Publication date: April 6, 2017Inventor: Marco Pieri
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Publication number: 20170003109Abstract: A tool to measure the radial stacking angle of a cylindrical blade comprises a base configured to indicate a radial direction of the hub, a component slidable over the blade and configured to indicate the stacking direction of the cylindrical blade, reference elements to provide a reference scale, a setting element configured to set the position of the component with respect to the base, a marker element configured to indicate the magnitude of the angle between the stacking direction and the radial direction using the reference elements; the angle corresponds to the radial stacking angle.Type: ApplicationFiled: November 28, 2014Publication date: January 5, 2017Inventor: Marco PIERI
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Patent number: 9422820Abstract: A system includes a turbomachine that includes at least one rotor disk or stage having a peripheral portion disposed about a rotational axis of the rotor disk or stage. The peripheral portion includes a groove that extends circumferentially about the peripheral portion. The groove has a first groove surface and a second surface disposed opposite the first groove surface. The turbomachine also includes a closure bucket disposed adjacent at least one bucket within the groove. The closure bucket has a first surface that interfaces with the first groove surface and a second groove surface disposed opposite the first surface. The closure bucket blocks circumferential movement of the at least one bucket within the groove relative to the rotor disk or stage. The turbomachine further includes a single wedge disposed between and contacting the second surface of the closure bucket and the second groove surface to secure the closure bucket within the groove.Type: GrantFiled: May 2, 2013Date of Patent: August 23, 2016Assignee: NUOVO PIGNONE SRLInventor: Marco Pieri
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Publication number: 20150027212Abstract: A system and method for monitoring and diagnosing anomalies in an output of a gas turbine, the method including storing a plurality rule sets specific to a performance of the gas turbine. The method further including receiving real-time and historical data inputs relating to parameters affecting the performance of the gas turbine, periodically determining current values of the parameters, comparing the initial values to respective ones of the current values, determining a degradation over time of the at least one of the performance of the compressor, the power output, the heat rate, and the fuel consumption based on the comparison, recommending to an operator of the gas turbine a set of corrective actions to correct the degradation.Type: ApplicationFiled: March 1, 2013Publication date: January 29, 2015Applicant: Nuovo Pignone SrlInventors: Ever Avriel Fadlun, Abdurrahman Abdalah Khalidi, Marco Pieri, Arul Saravanapriyan, Osama Naim Ashour
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Publication number: 20140205460Abstract: A system includes a turbomachine that includes at least one rotor disk or stage having a peripheral portion disposed about a rotational axis of the rotor disk or stage. The peripheral portion includes a groove that extends circumferentially about the peripheral portion. The groove has a first groove surface and a second surface disposed opposite the first groove surface. The turbomachine also includes a closure bucket disposed adjacent at least one bucket within the groove. The closure bucket has a first surface that interfaces with the first groove surface and a second groove surface disposed opposite the first surface. The closure bucket blocks circumferential movement of the at least one bucket within the groove relative to the rotor disk or stage. The turbomachine further includes a single wedge disposed between and contacting the second surface of the closure bucket and the second groove surface to secure the closure bucket within the groove.Type: ApplicationFiled: May 2, 2013Publication date: July 24, 2014Applicant: General Electric CompanyInventor: Marco Pieri